TCDS 1A15

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A15 Revision 34 Piper Aircraft, Inc PA-24 PA-24-250 PA-24-260 PA-24-400 August 7, 2006 AIRCRAFT SPECIFICATION NO. 1A15 Type Certificate Holder Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 Type Certificate Holder Record The New Piper Aircraft, Inc transferred TC 1A15 to Piper Aircraft, Inc on August 7, 2006 I. - Model PA-24, 4 PCLM (Normal Category), Approved June 20, 1957. Engine Lycoming O-360-A1A (See Item 111 for eligible relocated engines) Fuel 91/96 min. grade aviation gasoline Engine Limits All operations, 2700 r.p.m. (180 hp) Airspeed Limits Vne (Never Exceed) 202 mph (175 knots) Vno (Maximum Structural Cruise) 160 mph (139 knots) Vp (Maneuvering) 154 mph (134 knots) Vfe (Flaps Extended) 125 mph (108 knots) Vle (Landing Gear Extended) S/N 24-2 through 24-102: 125 mph (108 knots) S/N 24-1, and 24-103 through 24-3687: 150 mph (130 knots) Center of Gravity (+89.0) to (+94.0) at 2550 lb. (C. G.) Range (+83.0) to (+94.0) at 2206 lb. (Gear Extended) (+82.0) to (+94.0) at 1900 lb. or less Straight line variation between points given. Moment due to retracting of landing gear (1266 in. -lb.) Aircraf t Weight (lb.) 2550 2206 1900 Inches Aft of Datum 94.089.0 83.0 82.0 Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 Rev. No. 34 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 33 Page No. 25 26 27 28 Rev. No. 33 33 33 33 1A15 Page 2 of 28 Empty Weight C. G. Range None Maximum Weight 2550 lb. Number of Seats 4 (2 at +85, 2 at +118.5) Maximum Baggage Rear compartment at (+142) 100 lb. (S/N 24-2 through 24-102) 200 lb. (S/N 24-1, and 24-103 through 24-3687) Fuel Capacity 60 gallons at (+90) (Two wing tanks) Oil Capacity 2 gallons at (+25) (+24 when Item 111 is installed.) Control Surface Movements Main Surfaces Aileron 19° Up 15° Down Horizontal T.E. S/N 24-2 through 24-102: 11° Up 5° Down S/N 24-1, 24-103 through 24-3687: 13° Up 5° Down Rudder 25° Left 25° Right Flap 27° Down Anti-Servo tab (with stabilizer in neutral position) 7° Up 13° Down Serial Numbers Eligible 24-1 through 24-3687. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a), 1(b), 101, 102, 103, 201(a), 205, 206(a), 301(a), 302(a), and 401(a), 401(d) or 401(k). II. - Model PA-24-250, 4 PCLM (Normal Category), Approved April 16, 1958. Engine Lycoming O-540-A1A (See Item 109 for optional engines) Fuel 91/96 min. grade aviation gasoline Engine Limits All operations, 2575 r.p.m. (250 hp) Airspeed Limits Vne (Never Exceed)*** 203 mph (177 knots) Vno (Maximum Structural Cruise) 180 mph (156 knots) Vle (Landing gear extended) 150 mph (130 knots) Vp (Maneuvering) 144 mph (125 knots) Vfe (Flaps Extended) 125 mph (108 knots) *** See Item 618 for approved speed increase. Page 3 of 28 1A15 Center of Gravity S/N 24-1, 24-103 through 24-2298, except 24-2003: (C.G.) range (+87.7) to (+93.0) at 2800 lb. (+82.5) to (+93.0) at 2400 lb. (+80.5) to (+93.0) at 1900 lb. S/N 24-2003, 24-2299 through 24-3687: (+86.0) to (+93.0) at 2900 lb. (+82.5) to (+93.0) at 2600 lb. (+80.5) to (+93.0) at 2000 lb. Straight line variation between points given. Moment due to retracting of landing gear (1266 in. -lb.) Aircraft Weight (lb.) 2900 2600 2000 Aircraft Weight (lb.) 280 0 240 0 19 00 93.087.7 82.5 80.5 Inches Aft of Datum 86.0 82.5 80.5 S/N 24-1, 24-103 through 24-2298 Except 24-2003 S/N 24-2003, 24-2299 through 24-3687 Inches Aft of Datum 93.0 Empty Weight C. G. Range None Maximum Weight 2800 lb. (S/N 24-1, 24-103 through 24-2298, except 24-2003) 2900 lb. (S/N 24-2003, 24-2299 through 24-3687) Number of Seats 4 (2 at +85, 2 at +118.5) Maximum Baggage 200 lb. at (+142) (Rear compartment) Fuel Capacity S/N 24-1, 24-103 through 24-2843, except 24-2563: 60 gallons at (+90) (Two 30 gallon wing tanks) S/N 24-2563, 24-2844 through 24-3687: 56 gallons at (+90) (Two 28 gallon wing tanks) See NOTE 1 for unusable fuel. See Item 112 for auxiliary fuel tanks. Oil Capacity 3 gallons at (+28) Control Surface Movements Main Surfaces Aileron 19° Up 15° Down Horizontal T.E. S/N 24-1, 24-103 through 24-2843, except 24-2563: 13° Up 5° Down S/N 24-2563, 24-2844 through 24-3687: 14° Up 4° Down Rudder 25° Left 25° Right Flap S/N 24-1, 24-103 through 24-2843 except 24-2563: 27° Down S/N 24-2563, 24-2844 through 24-3687: 32° Down 1A15 Page 4 of 28 Control Surface Movements Anti-Servo tab (with stabilizer in neutral position) S/N 24-1, 24-103 through 24-2843, except 24-2563: 7° Up 13° Down S/N 24-2563, 24-2844 through 24-3687: 7° Up 15° Down Serial Numbers Eligible 24-1, 24-103 through 24-3687. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 3(a) and 3(b), 103, 106, 107(a) or 107(b), 201(a), 202(b), 205, 206(a), 301(a) or 301(b), 302(a), 401(c), or 401(f), or 401(n), or 401(s), or 401(v), 603, 617(a), 401(bz) When Item 109(e) is installed, substitute Items 113 and 114(a) or 114(b) in place of Items 106 and 107(a) or 107(b), respectively. III. Model PA-24-400, 4 PCLM (Normal Category), Approved December 27, 1963. Engine Lycoming IO-720-A1A or IO-720-A1B Fuel 100/130 min. grade aviation gasoline Engine Limits All operations, 2650 r.p.m. (400 hp) Airspeed Limits Vne (Never Exceed) 250 mph (219 knots) Vno (Maximum Structural Cruise) 210 mph (182 knots) Vp (Maneuvering) 160 mph (139 knots) Vle (Landing Gear Extended) 150 mph (130 knots) Vfe (Flaps Extended) 125 mph (108 knots) Center of Gravity (+84.8) to (+90) at 3600 lb. (C. G.) Range (+81.5) to (+90) at 3300 lb. (Gear Extended) (+77.0) to (+90) at 2500 lb. or less Straight line variation between points given. Moment due to retracting of landing gear (1266 in. -lb.) Aircra ft Weight (lb.) 3600 3300 2500 Inches Aft of Datum 90.084.8 81.5 77.0 Empty Weight C. G. Range None Maximum Weight 3600 lb. Page 5 of 28 1A15 Number of Seats 4 (2 at +85, 2 at +118.5) (S/N 26-2 through 26-124) 4 (2 at +85, 2 at +120.5) (S/N 26-125 through 26-148) Maximum Baggage 200 lb. at (+142) (Rear compartment) Fuel Capacity 130 gallons at (+90) (Two 30 gallon wing tanks) (124 gallons usable) 130 gallons at (+94) (Two 35 gallon wing tanks) (124 gallons usable) See NOTE 1 for unusable fuel data. Oil Capacity 17 quarts at (+21) (12 quarts usable) Control Surface Main Surfaces Aileron 19° Up 15° Down Movements Stabilator (L.E.) 4.5° Up 15.5° Down Rudder 25° Left 25° Right Flap 38° Down Anti-Servo Tab (Stabilizer Neutral) 4.5° Up 9° Down Serial Numbers Eligible 26-2 through 26-148. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 7(a), 7(b), 115, 116, 118, 119, 201(c), 205, 206(b), 302(a), 305, 401(ag), 603, and 605. IV. Model PA-24-260, 4 PCLM (Normal Category), Approved June 19, 1964, or 6 PCLM (Normal Category), Approved June 30, 1965, and April 11, 1969 when Item 611 is installed (See NOTE 2(m) placard for 6 PCLM Limitations.). Engine Lycoming O-540-E4A5 (See Item 109(f) and 109(g) for additional optional engines and 109(h) for optional turbocharged engines) Fuel 91/96 min. grade aviation gasoline (normally aspirated engine) 100/130 min. grade aviation gasoline (turbocharged engine) Engine Limits All operations, 2700 r.p.m. (260 hp) Airspeed Limits Vne (Never Exceed)*** 203 mph (177 knots) Vno (Maximum Structural Cruise) 180 mph (156 knots) Vle (Landing Gear Extended) 150 mph (130 knots) Vp (Maneuvering) 144 mph *(125 knots) Vfe (Flaps Extended) 125 mph (108 knots) Vp (Maneuvering) 150 mph **(130 knots) * S/N 24-3642, 24-4000 through 24-4782, and 24-4784 through 24-4803. ** S/N 24-4783, 24-4804 through 24-5034. *** See Item 618 for approved speed increase. 1A15 Page 6 of 28 Center of Gravity S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299: (C. G.) Range (+86.0) to (+93.0) at 2900 lb. (Gear Extended) (+82.5) to (+93.0) at 2600 lb. (+80.5) to (+93.0) at 2000 lb. or less Straight line variation between points given. Moment due to retracting of landing gear (1266 in. -lb.) 2000 2600 2900 Inches Aft of Datu m 80.5 86.082.5 93.0 24-478 3 04 S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803: (+88.4) to (+93.0) at 3100 lb. (+82.5) to (+93.0) at 2600 lb. (+80.5) to (+93.0) at 2000 lb. or less S/N 42-4783, and 24-4804 through 24-5034 (with normally aspirated engine only): (+89.6) to (+93.0) at 3200 lb. (+82.5) to (+93.0) at 2600 lb. (+80.5) to (+93.0) at 2000 lb. or less Straight line variation between points given. Moment due to retracting of landing gear (1266 in. -lb.) 3200 Serial No. and 24-48 2000 2600 3100 Aircra ft Weight (lb.) Serial No. 24-4247; 24-4300 through 24-4782; 24-4784 through 24-4 803. In ches Aft of Datum 80.5 82.5 88.4 89.6 93.0 through 24-5034 Page 7 of 28 1A15 Center of Gravity S/N 24-4783, and 24-4804 through 24-5034 (with turbocharged engines only): (C. G.) Range (+87.6) to (+93.0) at 3200 lb. Gear Extended (+83.2) to (+93.0) at 2800 lb. (+80.5) to (+93.0) at 2000 lb. or less Straight line variation between points given. Moment due to retracting of landing gear (1266 in. -lb.) 2000 2800 3200 80.5 83.2 87.6 93.0 Aircraft Weight (lb.) Inches Aft of Datum Empty Weight C. G. Range None Maximum Weight S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299: 2900 lb. S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803: 3100 lb. - Takeoff 2945 lb. - Landing S/N 24-4783, and 24-4804 through 24-5034: 3200 lb. - Takeoff 3040 lb. - Landing Number of Seats 4 (2 at +85, 2 at +120.5) S/N 24-4247, and 24-4300 through 24-5034 when Item 611 is installed: 6 (2 at +85, 2 at +120.5, 2 at +148) Maximum Baggage S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299: 200 lb. at (+142) (Rear compartment) S/N 24-4247, and 24-4300 through 24-5034: 250 lb. at (+142) (Max. baggage and/or passenger allowance in baggage area, including seats) Fuel Capacity 56 gallons at (+90) (Two 28 gallon wing tanks) See NOTE 1 for unusable fuel. See Item 112 for auxiliary fuel tanks. Oil Capacity 3 gallons at (+28) Control Surface Main Surfaces Aileron 19° Up 15° Down Movements Stabilator (L.E.) 14° Up 4° Down Rudder 25° Left 25° Right Flap 32° Down Anti-Servo Tab (Stabilizer Neutral) 7° Up 15° Down 1A15 Page 8 of 28 Serial Numbers Eligible 24-3642, 24-4000 through 24-5034. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: S/N 24-3642, 24-4000 through 24-4246, and 24-4248 through 24-4299: 4(b), 9(a) or 9(c), 9(b), 103, 106, 107(c), 107(d) or 107(e), 201(d), 202(b), 205, 206(a), 302(a), 305, 401(ah), 603, 617(a), and 401(bz). When Item 109(f) is installed, substitute Items 113 and 114 and 401(ak) in place of Items 106, 107(c), 107(d), or 107(e), and 401(ah), respectively. S/N 24-4247, 24-4300 through 24-4782, and 24-4784 through 24-4803: 4(b), 9(a), 9(b), 103, 106, 107(e), 201(d), 202(b), 205, 206(a), 124, 305, 401(av), 603, 617(a), and 401(bz). When Item 109(f) is installed, substitute Items 113, 114(d), and 401(ba) in place of 106, 107(e), and 401(av), respectively. S/N 24-4783, and 24-4804 through 24-5034 (with normally aspirated engine): 9 (b), 9(d) or 9(g), (9e), 109(g), 113, 114(d), 120(a) or 120(c), 201(d), 202(b), 205, 206(a), 302(a), 305(c), 401(bo), 603, 617(a), and 410(bz). S/N 24-4783, and 24-4804 through 24-5034 (with turbocharged engine): 9(b), 9(f) or 9(h), 9(e), 109(h), 115, 120(b), 121(a), 122(a), 201(d), 202(b), 205, 206(a), 124, 302(a), 305(c), 401(bp), 603, 616(a), 617(a), and 401(bz). Specifications Pertinent to All Models Datum 79 in. ahead of the wing leading edge at Wing Station 65.5 (intersection point of tapered edge with straight leading edge). Leveling Means Level from two rivnuts located right side above baggage door. On S/N 24-4247, and 24-4300 through 24-5034 still on right side of fuselage, but baggage door moved to left side of fuselage. Certification Basis Type Certificate No. 1A15 (CAR 3, effective November 1, 1949, including Amendments 3-1 through 3-12, effective April 13, 1954). Production Basis Approved for manufacture of spare parts only under Production Certificate No. 206. Equipment: A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. Propeller and Propeller Accessories PA-24 PA-24-250 PA-24-400 PA-24-260 1. (a) Propeller - Hartzell constant speed controllable, hub model HC92ZK-8D, blades model 8447A-12A Pitch: High 27°, Low 13° at 30 in. station Diameter Not over 72¼ in., not under 70.5 in. 63 lb. (+3) - - - - - - - - - - - - (b) Governor Assembly: Woodward 210185, 210260, 210305, or Hartzell D1-1, D1-5. 5 lb. (+39) - - - - - - - - - - - - (c) Deleted May 5, 1958. (Included in Item 4) Page 9 of 28 1A15 Propeller and Propeller Accessories (cont.) PA-24 PA-24-250 PA-24-400 PA-24-260 2. (a) Propeller - McCauley constant speed controllable, hub model 2D36C14, blades model 78KM-4. Pitch: High 27.5°, Low 12.7° at 30 in. station Diameter: Not over 74 in., not under 72 in. Item 401(b) or 401(1) required. 60 lb. (+3) - - - - - - - - - - - - (b) Governor Assembly: Woodward 210185, 210250, 210260, 210305 or Hartzell D1-1, D1-5. 5 lb. (+39) - - - - - - - - - - - - 3. (a) Propeller - Hartzell constant speed controllable, hub model HC82XK-1D or HC-A2XK-1, blades model 8433-7, or hub Model HC-A2VK-1, blades Model V8433N-7. Pitch: High 31° to 33°, Low 14.5° at 30 in. station Diameter: Not over 77 7/16 in., not under 76 in. Placard required: (For O-540-A1A engine only) "Avoid continuous operation between 2225 and 2275 r.p.m." 63 lb. - - - - (+1.5) - - - - - - - - (b) Governor Assembly: Woodward 210185 or 210250 or Hartzell B-4-2. 5 lb. - - - - (+10) - - - - - - - - 4. (a) Hartzell spinner dome C-888 and bulkhead adapter C-885 (Eligible on Items 1(a) and 3(a) only) 3 lb. (+3) (+1.5) - - - - - - - - (b) Piper spinner dome and bulkhead adapter 3 lb. (+3) (+1.5) - - - -- (+1.5) 5. (a) Propeller - McCauley constant speed controllable, hub model 2D36C28, blades model 80MM-6. Pitch: High 32°, Low 15.7° at 30 in. station Diameter: Not over 74 in., not under 73 in. Placard required: (For O-540-A1A engine only) "Avoid continuous operation between 2225 and 2275 rpm." Item 401(e), 401(g) or 401(o) required. 60 lb. - - - - (+1.5) - - - - - - - - (b) Woodward hydraulic governor assembly Model A210185 per Piper Dwg. 21764-3 or Model A210305 per Piper Dwg. 21764-4 when Item 5(a) is installed. 5 lb. - - - - (+10) - - - - - - - - 6. Deleted October 24, 1960. 7. (a) Propeller - Hartzell constant speed controllable, hub model HC-A3VK-4, blades model V8433-7. Pitch: High 36°, Low 14° at 30 in. station Diameter: Not over 77 5/8 in., not under 75 5/8 in. See NOTE 2(k) 88 lb. - - - - - - - - (-3.5) - - - - (b) Governor Assy. - Hartzell F-4-1 per Piper Dwg. 24622-2. 6 lb. - - - - - - - - (+3.5) - - - - 8. Spinner Dome per Piper Dwg. 22752-2 and spinner Bulkhead Adapter per Piper Dwg. 22774-2. 4 lb. - - - - - - - - (-3.5) - - - - 1A15 Page 10 of 28 Propeller and Propeller Accessories (cont.) PA-24 PA-24-250 PA-24-400 PA-24-260 9. (a) Propeller - Hartzell constant speed controllable, hub model HC-C2YK-1A, blades model 8467-7R. Pitch: High 32° to 34°, Low 15° at 30 in. station Diameter: Not over 77 in., not under 75 in. NOTE: If it becomes necessary to reduce the propeller diameter below 77 inches, for maintenance or rebalancing purposes, a placard stating "Avoid continuous operation between 2500 and 2600 r.p.m. above 25 inch manifold pressure" must be displayed near the manifold pressure gauge. 54 lb. (+1.5) (b) Governor Assy. Hartzell F-4-4 per Piper Dwg. No. 24622-5 or F-4-4A per Piper Dwg. No. 24622-10 6 lb. - - - - - - - - - - - -- (+10) (c) Propeller - Hartzell constant speed controllable, hub model HC-C2YK-1B, blades model 8467-7R Pitch: High 32° to 34°, Low 15° at 30 in. station Diameter: Not over 77 in., not under 75 in. NOTE: If it becomes necessary to reduce the propeller diameter below 77 inches, for maintenance or rebalancing purposes, a placard stating "Avoid continuous operation between 2500 and 2600 r.p.m. above 25 inch manifold pressure", must be displayed near the manifold pressure gauge. 56 lb. - - - - - - - - - - - - (+1.5) (d) Propeller - Hartzell constant speed controllable, hub model HC-E2YR-1B, blades model 8467-7R Pitch: High 32° to 34°, Low 15° at 30 in. station Diameter: Not over 77 in., not under 75 in. 59 lb. - - - - - - - - - - - - (-3.4) (e) Spinner dome Piper P/N 26326 with bulkhead adapter Piper P/N 26313 4 lb. - - - - - - - - - - - - (-4.1) (f) Propeller - Hartzell constant speed controllable, hub model HC-E2YR-1B, blades model 8467-7R Pitch: High 32° to 34°, Low 13.5° (+.3°, -0°) at 30 in. station Diameter: Not over 77 in., not under 75 in. 59 lb. - - - - - - - - - - - - (-3.4) (g) Propeller - Hartzell constant speed controllable, hub Model HC-E2YR-1BF, blades Model F8467-7R Pitch: High 32° to 34°, Low 15° at 30 in. station Diameter: Not over 77 in., not under 75 in. 59 lb. - - - - - - - - - - - - (-3.4) (h) Propeller - Hartzell constant speed controllable, Hub Model HC-E2YR-1BF, Blades Model F8467-7R Pitch: High 32° to 34°, Low 13.5° (+.3°, -0°) at 30 in. station Diameter: Not over 77 in., not under 75 in. 59 lb. - - - - - - - - - - - - (-3.4) (i) Spinner Dome and Bulkhead Installation per Piper Kit 760-452. 5 lb. - - - - - - - - - - - - (+1.5) Page 11 of 28 1A15 Engine and Engine Accessories - Fuel and Oil System PA-24 PA-24-250 PA-24-400 PA-24-260 101. Fuel pump, electric auxiliary, Bendix Model 476087 or 478360 2 lb. (+38) - - - - - - - - - - - - 102. Fuel pump, engine-driven (a) AC No. 5594068 3 lb. (+33) - - - - - - - - - - - - (b) AC No. 5623467 (Lycoming P/N 74060), AC No. 5656880 (Lycoming P/N 74082) or AC No. 6440295 (Lycoming P/N 75246) 1.5 lb. (+33) - - - - - - - - - - - - 103. Oil radiator, Harrison Model AP07AU06-03 3 lb. (+12) (+10.5) - - - - (+10.5) 104. Starter, Delco-Remy, Model 1109673 or 1109689, 12 volt geared (2.27:1) 19 lb. (+15) - - - - - - - - - - - - 105. Vacuum pump (a) Pesco Model 3P-194-F Type B-11 4 lb. (+33) (+39) - - - - - - - - (b) Deleted February 12, 1959 (c) Garwin G-455L 4 lb. (+33) (+39) - - - - - - - - (d) Airborne Mechanisms 113A1, 113A5 or 200CC 4 lb. (+33) (+39) (+43) (+39) 106. 2 fuel pumps, elec. aux. Bendix Model 476087 or 478360. Required except when Item 109(e) or 109(f) is installed. 2 lb. each - - - - (+43) - - - - (+60) 107. Fuel pump, engine-driven Required except when Item 109(e) or 109(f) is installed. (a) AC No. 5594605 4 lb. - - - - (+39.5) - - - - - - - - (b) AC No. 5623467 (Lycoming P/N 74060 ) or AC No. 5656880 (Lycoming P/N 74082) 1.5 lb. - - - - (+39.5) - - - - - - - - (c) AC No. 6440152 (Lycoming P/N 74798) 1.5 lb. - - - - - - - - - - - - (+39.5) (d) AC No. 6440174 2 lb. - - - - - - - - - - - - (+39.5) (e) AC No. 6440295 2 lb. - - - - - - - - - - - - (+39.5) 108. (a) Starter, Delco-Remy Model 1109695, 1109504, or 1109511; 12 Volt, Geared 3.38:1. Model 1109511 is eligible for installation on Model PA-24-260 only. 18 lb. - - - - (+13.5) - - - - (+13.5) (b) Starter, Prestolite Model MZ-4206, 12 Volt, Geared 3.38:1 17 lb. - - - - - - - - - - - - (+13.5) 109. Optional engines (Lycoming) (a) O-540-A1A5 (Item 401(f) and 401(n) required) Neg.Wt.Ch. - - - - Elig. - - - - - - - - (b) O-540-A1B5 (Item 401(f) and 401(n) required) Neg.Wt.Ch. - - - - Elig. - - - - - - - - (c) O-540-A1C5 (Item 401(f) and 401 (n) required) Neg.Wt.Ch. - - - - Elig. - - - - - - - - (d) O-540-A1D5 (Item 401(f), 401(n) and 401(s) required) Neg.Wt.Ch. - - - - Elig. - - - - - - - - (e) IO-540-C1B5 (Fuel injection installed per Piper Dwg. No. 23144) (Items 113, 114(a) or 114(b) and 401(v) required). Neg. Wt.Ch. - - - - Elig. - - - - - - - - (f) IO-540-D4A5 (Fuel injection installed per Piper Dwg. No. 24923) (Items 113, 114 and 401(ak) or 401(ba) required). Use Actual Wt. Ch. - - - - - - - - - - - - Elig. 1A15 Page 12 of 28 Engine and Engine Accessories - Fuel and Oil System (cont.) PA-24 PA-24-250 PA-24-400 PA-24-260 109. (g) IO-540-N1A5 Use Actual Wt. Chg. - - - - - - - - - - - - Elig. ` (h) IO-540-R1A5 (Turbocharged - Items 122(a) required) installed per Piper Dwg. 27137 Use Actual Wt. Chg. - - - - - - - - - - - - Elig. 110 Carburetor air filter, Fram Paper Filter No. CA-161-PL Neg.Wt.Ch. Elig. Elig. - - - - Elig. 111. Engine relocated per Piper Dwg. No. 22000. Eligible on Model PA-24, S/N 24-1684 through 24-3687. Item 401(k) required. Use Actual Wt. Change Elig. - - - - - - - - - - - - (a) Lycoming O-360-A1A (b) Lycoming O-360-A1D (Limits same as for O-360-A1A) The following is the new arm aft of datum for each item of equipment that is relocated when Item 111 is installed: Item Arm Item Arm 1(a) (+1.5) 102 (+32.5) 1(b) (+35) 103 (+10.5) 2(a) (+1.5) 104 (+13.5) 2(b) (+35) 105 (+31.5) 4 (+1.5) 301(a) (+11.5) 6(a) (+1.5) 301(b) (+11.5) 6(b) (+35) PA-24 PA-24-250 PA-24-400 PA-24-260 112. Two 15 gallon auxiliary wing fuel tanks. Eligible on Models PA-24-250 and PA-24-260, S/N 24-2003, 24-2299 through 24-5034. 13 lb. - - - - (+97) - - - - (+97) 113. Fuel Pump, boost, rotary, motor-driven (a) Bendix No. 480518-1 or 480528 5 lb. - - - - (+60) - - - - (+60) (b) Dukes No. 4140-00-218 Required with Items 109(e), 109(f) and 109(g). 2 lb. - - - - (+60) - - - - (+60) 114. Fuel Pump - Engine Driven. Required with Items 109(e) and 109(f). (a) AC No. 5656696A 2 lb. - - - - (+39.5) - - - - (+39.5) (b) AC No. 6440160 (Lycoming No. 74999) 2 lb. - - - - (+39.5) - - - - (+39.5) (c) AC No. 5656999 (Lycoming No. 75131) 2 lb. - - - - - - - - - - - - (+39.5) (d) AC No. 6440296 2 lb. - - - - - - - - - - - - (+39.5) 115. Fuel Pump, engine driven, Lear Siegler No. RG17980, Lycoming No. 74547 1 lb. - - - - - - - - (+43) (+39.5) 116. Oil radiator, 2 required, Harrison Model AP13AU06-01 3 lb. ea - - - - - - - - (+39) - - - - 117. Starter, Delco-Remy Model 1113471, Lycoming No. 72279, 12V, geared 3.00:1 35 lb. - - - - - - - - (+12) - - - -- 118. Induction air filter, Fram Paper Filter No. CA-173PL 1 lb. - - - - - - - - (+10) - - - - 119. (a) Fuel pump, boost rotary motor-driven, Bendix No. 480533 5 lb. - - - - - - - - (+60) - - - - (b) Fuel pump-boost-elec. Airborne Mfg. Co. No. 2B6-26. 3.7 lb. - - - - - - - - (+60) - - - - Page 13 of 28 1A15 Engine and Engine Accessories - Fuel and Oil System (cont'd) PA-24 PA-24-250 PA-24-400 PA-24-260 120. (a) Oil radiator - Harrison Model AP09AU06-02, Piper P/N 16943 2.4 lb. - - - - - - - - - - - - (+45.8) (b) Harrison Model AP18AU06-03, Piper P/N 43378 3.6 lb. - - - - - - - - - - - - (+45.8) (c) Harrison Model AP09AU06-04, Piper P/N 32912 2.4 lb. - - - - - - - - - - - - (+45.8) 121. (a) Fuel Pump, elec. aux. (boost) Dukes No. 4140-00-SPC 2 lb. - - - - - - - - - - - - (+60) 122. (a) Turbocharger Rayjay No. RJ0080-102 (2 required when Item 109(h) is installed) 13.5 lb. ea - - - - - - - - - - - - (+26.0) 123. Manually Controlled Heated Alternate Engine Induction Air System (a) Installation per Piper Dwg. 27186 3 lb. - - - - - - - - - - - - (+27.2) Placards in NOTE 2(w) are required. (Eligible S/N 24-3642, 24-4000 through 24-4299, except 24-4247. Item 401(bv) required.) (Eligible S/N 24-4247, 24-4300 through 24-4803, except 24-4783. Item 401(bw) required.)